Thrust generating apparatus

a technology of thrust generating apparatus and thrust cylinder, which is applied in the direction of piston pump, marine propulsion, vessel construction, etc., can solve the problems of diesel engine air pollution in terms of environmental performance, and achieve the effects of improving the strength of the propeller blade, improving maintenance efficiency, and easy replacemen

Inactive Publication Date: 2012-08-09
KAWASAKI HEAVY IND LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Benefits of technology

[0011]According to the above configuration, a radially outer portion of the propeller blade is fixed to the rotor main body, and a radially inner portion of the propeller blade is fixed to the boss. Therefore, the strength of the propeller blade imp

Problems solved by technology

However, it has been pointed out that the diesel engine has a

Method used

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  • Thrust generating apparatus
  • Thrust generating apparatus
  • Thrust generating apparatus

Examples

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embodiment 1

[0020]As shown in FIGS. 1 and 2, a thrust generating apparatus 10 of Embodiment 1 includes: an annular stator 11 fixed to a hull; an annular rotor 12 capable of rotating positively and negatively relative to the stator 11; a propeller member 13 formed integrally with the rotor 12 on a radially inner side of the rotor 12; and a boss 14 formed integrally with a radially inner tip end of the propeller member 13 and provided on a rotation axis line X of the rotor 12.

[0021]The stator 11 includes an annular outer casing 21 and an annular inner casing 22 provided on an inner periphery side of the outer casing 21. A substantially cylindrical space formed between the outer casing 21 and the inner casing 22 is a cooling space S1. The outer casing 21 is a cylindrical duct on which a cable through hole 21a is partially formed. The cable through hole 21a is closed by a lid 23. The inner casing 22 is formed by coupling first to fourth casings 24 to 27, support rings 28 and 29, and fairings 30 and...

embodiment 2

[0039]As shown in FIGS. 4 and 5, a stator 111 of a thrust generating apparatus 110 of Embodiment 2 includes an annular outer casing 121 and an annular inner casing 22 provided on an inner periphery side of the outer casing 121. A cylindrical space formed between the outer casing 121 and the inner casing 22 is the cooling space S 1. The outer casing 121 includes: a casing main body 130 including an upper surface opening 130i; and a cover 131 configured to close the upper surface opening 130i of the casing main body 130. Since components of the thrust generating apparatus 110 are the same as those of Embodiment 1 except for the outer casing 121, the same reference signs are used for the same components, and detailed explanations thereof are omitted.

[0040]The casing main body 130 includes: vertical wall portions 130a and 130b opposed to each other in the left-right direction; inner cylindrical portions 130d and 130e, each of which projects in the outward direction along the rotation ax...

embodiment 3

[0042]As shown in FIGS. 6 and 7, according to the thrust generating apparatus of Embodiment 3, the propeller blades of a propeller member 113 can be disassembled individually. Since the components except for the propeller member 113 and a boss 114 are the same as those of Embodiment 1 or 2, explanations thereof are omitted.

[0043]The propeller member 113 is constituted by assembling a plurality of (for example, six) separable propeller members 170. Each of the separable propeller members 170 includes: a circular-arc plate portion 170a on which bolt holes 170d are formed; a propeller blade 170b projecting in the radially inward direction from the circular-arc plate portion 170a ; and a stopper protrusion portion 113c projecting in the radially inward direction from a radially inward tip end of the propeller blade 170b.

[0044]The boss 114 includes a pair of separable bosses 151 and 152 configured to be separable in both directions along the rotation axis line X. Each of the separable b...

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Abstract

A thrust generating apparatus is provided under water and configured to generate thrust by ejecting the water. A rotor main body includes: a first member including a side surface and outer peripheral surface which are opposed to a first water lubricated bearing; a second member including a side surface and outer peripheral surface which are opposed to a second water lubricated bearing; and a third member including a supporting surface contacting an inner peripheral surface of a rotor core. The first to third members are fixed to one another so that each member is detachable.

Description

RELATED APPLICATION[0001]This application claims priority to and the benefit of Japanese Patent Application No. 2009-150523, filed in Japan Patent Office on Jun. 25, 2009, the entire disclosure of which is incorporated herein by reference.TECHNICAL FIELD[0002]The present invention relates to a thrust generating apparatus configured to generate propulsive force of, for example, a vessel.BACKGROUND ART[0003]In recent years, due to shortage of energy resources and the like, it has been required to improve the efficiency of a propulsion system configured to generate a propulsive force in a vessel. In the propulsion system of the vessel, a diesel engine has the most excellent heat efficiency among various prime movers, and the propulsion system in which the diesel engine is coupled directly or via a reducer to a propeller as a propulsor is now the mainstream. However, it has been pointed out that the diesel engine has an air pollution problem in terms of environmental performance. As an ...

Claims

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Application Information

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IPC IPC(8): F04D13/06
CPCB63H1/16B63H23/24B63H21/17B63H2023/005B63H1/12B63H25/42
Inventor TANAKA, MASAHITOKIYOSE, HIROMITSUIKEBUCHI, TETSURONAKAGAWA, KENTARO
Owner KAWASAKI HEAVY IND LTD
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